Hypersonic Shock-heated Flow Parameters for Velocities to 46,000 Feet Per Second and Altitudes to 323,000 Feet PDF Download
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Author: Paul William Huber
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88
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Book Description
Real-air hypersonic-flow parameters are presented in tabular and graphical form for flight in the earth's atmosphere as a function of flight velocity and flight altitude. Thermochemical equilibrium-flow properties are given for the inviscid normal shock and stagnation point, and both equilibrium and frozen-flow parameters, including electron concentration, are listed for the far wake of the inviscid stagnation streamline. Plots of electron collision frequency and electrical conductivity in the normal shock and wake plasmas are also included. The tabulations are made for twelve flight altitudes, ranging from 35,900 feet to 322,900 feet and for flight velocities and shock-heated gas temperatures encompassing those encountered in return from planetary missions. Included are discussions of the applicability of the computed parameters to a given problem, and effects due to the uncertainties in the input data for ambient air.
Author: Paul William Huber
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88
Get Book
Book Description
Real-air hypersonic-flow parameters are presented in tabular and graphical form for flight in the earth's atmosphere as a function of flight velocity and flight altitude. Thermochemical equilibrium-flow properties are given for the inviscid normal shock and stagnation point, and both equilibrium and frozen-flow parameters, including electron concentration, are listed for the far wake of the inviscid stagnation streamline. Plots of electron collision frequency and electrical conductivity in the normal shock and wake plasmas are also included. The tabulations are made for twelve flight altitudes, ranging from 35,900 feet to 322,900 feet and for flight velocities and shock-heated gas temperatures encompassing those encountered in return from planetary missions. Included are discussions of the applicability of the computed parameters to a given problem, and effects due to the uncertainties in the input data for ambient air.
Author: Paul William Huber
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 722
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Book Description
Author: Paul William Huber
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages :
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Book Description
Author: Lloyd S. Keafer
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 40
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Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 666
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Book Description
Author: John David Anderson
Publisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710
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Book Description
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Author: Ernest V. Zoby
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 58
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Book Description
Author: P. D. Fisher
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 60
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Book Description
This report presents in graphical form the stagnation point pressure, temperature, equilibrium surface temperature, and heating rate for a sphere. Equilibrium real-gas effects and surface radiation are considered. The charts cover a range of velocities from 0 to 15,000 feet per second and altitudes from sea level to 200,000 feet. Corrections for sphere diameter and emissivity are included. (Author).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 416
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Book Description
